S5.1
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Isayev Nitric acid/Amine rocket engine. SAM-missiles 217M and 218. Out of Production. Designation unknown.
Throttled thrust(vac): 49.000 kN (11,015 lbf). Engine: 122 kg (268 lb). Propellant Formulation: AK27I/TG-02. Thrust to Weight Ratio: 139.34.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- 217 missile
- Propellants
- Nitric acid/Amine
- Agency
- Isayev bureau